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ACAS X safety analysis in the current RTCA environment

机译:当前RTCA环境中的ACAS X安全分析

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The typical process for developing a safety analysis within the current RTCA environment is in the form of an Operational Safety Assessment (OSA) as specified in RTCA DO-264 [1]. This assessment is typically performed at a high level and is usually a qualitative analysis resulting in qualitative safety requirements. This OSA is often included in a Safety and Performance Requirements Document (SPR). The manufacturer of an avionics system would apply the requirements allocated to the aircraft systems to the product as part of the design. The next step in the safety process would be to perform a Functional Hazard Analysis (FHA) using the hazards for the system that can be caused by the avionics and perform a fault tree (FT) analysis on those hazards, identifying causes of the hazards related to the avionics system functions and showing that those causes lead to a top level hazard that meets the safety objective assigned to the hazard. This safety objective is stated in the SPR. The manufacturer would then take the requirements from the SPR and design the system architecture. TCAS II has a different history than what is stated above. TCAS II requirements are defined in the form of a MOPS document [2]. Safety analyses were performed on each version of TCAS II as it progressed. However, the safety studies were not part of the MOPS and were not readily archived for industry use. ACAS X is being designed as an improvement to TCAS II in the current RTCA environment. ACAS X is being defined by a MOPS document not an SPR. Due to the highly prescriptive nature of the ACAS X MOPS, like TCAS II, RTCA SC-147 should produce some of the documentation that would normally be produced by the manufacturers. The following proposal is an effective way to address the safety requirements of the current environment given the history of TCAS II. The following approach is proposed for the ACAS X safety analysis. Perform two related safety analyses for ACAS X: 1) a high level qualitative OSA i- the spirit of DO-264 [1] (or FHA defined by ARP 4761 [3]) which includes the elements of an OSED, OHA, and ASOR and 2) a safety gap analysis that defines safety concerns in ACAS X, describes what was performed in the TCAS II safety studies [4-10] and how this is applicable to ACAS X, and finally what work remains to be done to complete the ACAS X safety analysis. The OSA/FHA would result in hazards with qualitative safety objectives and qualitative safety requirements. The safety gap analysis would result in a collection of analyses, simulations, tests etc. to cover all of the safety concerns of the new system. This approach should satisfy the requirements of all the stakeholders involved in the implementation of ACAS X. It is recommended that these two safety analyses be included in the MOPS for ACAS X as Appendices.
机译:在当前RTCA环境中开发安全性分析的典型过程是RTCA DO-264中规定的操作安全评估(OSA)的形式[1]。该评估通常在高水平下进行,通常是定性分析,导致定性安全要求。此OSA通常包含在安全性和性能要求文件(SPR)中。航空电子系统制造商将应用于飞机系统的要求作为设计的一部分。安全过程中的下一步是使用可能由航空电子设备引起的系统的危害进行功能危害分析(FHA),并对这些危害进行故障树(FT)分析,识别相关的危险的原因向航空电子系统功能函数并表明这些原因导致符合分配给危害的安全目标的顶级危险。 SPR中的这种安全目标陈述。然后制造商将从SPR中获取要求并设计系统架构。 TCAS II具有与上述规定的历史不同的历史。 TCAS II要求以MOPS文件的形式定义[2]。当它进展时,对每个版本的TCAS II进行安全分析。然而,安全性研究不是拖把的一部分,并且不容易存档用于行业使用。 ACAS X正在设计为当前RTCA环境中TCAS II的改进。 ACAS X由MOPS文件定义而不是SPR。由于ACAS X MOP的高度规范性,如TCAS II,RTCA SC-147应该产生通常由制造商生产的文件。以下提议是鉴于TCAS II的历史,解决了当前环境的安全要求的有效方法。提出了以下方法,用于ACAS X安全性分析。对ACAS X执行两个相关的安全分析:1)高水平定性OSA I- DO-264 [1](或由ARP 4761定义的FHA定义的FHA),其中包括放置,OHA和ASOR的元素2)在ACAS X中定义安全问题的安全差距分析描述了在TCAS II安全研究中执行的内容[4-10]以及如何适用于ACAS X,最后仍有待完成的工作来完成ACAS X安全分析。 OSA / FHA将导致定性安全目标和定性安全要求的危害。安全差距分析将导致分析,模拟,测试等集合,以涵盖新系统的所有安全问题。这种方法应满足所有参与ACAS X的所有利益相关者的要求。建议将这两种安全分析包含在ACAS X的拖信中作为附录。

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